| 000 -LEADER |
|---|
| fixed length control field |
00620nam a22001817a 4500 |
| 003 - CONTROL NUMBER IDENTIFIER |
|---|
| control field |
OSt |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
|---|
| control field |
20210308124507.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
|---|
| fixed length control field |
210308b xxu||||| |||| 00| 0 eng d |
| 040 ## - CATALOGING SOURCE |
|---|
| Transcribing agency |
IIT Kanpur |
| 041 ## - LANGUAGE CODE |
|---|
| Language code of text/sound track or separate title |
eng |
| 100 ## - MAIN ENTRY--AUTHOR NAME |
|---|
| Personal name |
Mayo, Alton P. |
| 245 ## - TITLE STATEMENT |
|---|
| Title |
Matrix method for obraining spanwise moments and deflections of torsionally rigis rotor blades with arbitrary loadings [Technical Note 4304] |
| Statement of responsibility, etc |
Alton P. Mayo |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
|---|
| Place of publication |
Washington |
| Name of publisher |
National Advisory Committee for Aeronautics |
| Year of publication |
1958 |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Number of Pages |
51p |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
National Advisory Committee for Aeronautics (NACA) |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical Term |
matrix method |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Koha item type |
Reference |
